View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 40376U 26039.46390837 +.00000000 +00000-0 +14208-3 0 00001
2 40376 98.1306 48.3637 0001447 89.9493 270.1875 14.63438453 09
| Epoch (UTC): | 08 February 2026 11:08:01 |
| Eccentricity: | 0.0001447 |
| inclination: | 98.1306° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 48.3637° |
| argument of perigee: | 89.9493° |
| revolutions per day: | 14.63438453 |
| mean anomaly at epoch: | 270.1875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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